A Conceptual Design for the Space Launch Capability of the Peacekeeper ICBM

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This paper presents the results of the concept selection, refinement, and verification phases of the conceptual design for the space launch capability of the Peacekeeper Intercontinental Ballistic Missile (ICBM). The redesigned Peacekeeper Space Launch Vehicle (SLV) is intended to serve primarily as a rapid resupply system for the International Space Station (ISS). Using quality engineering techniques, many potential configurations were determined and evaluated based on performance, cost, availability, reliability, safety, commonality with existing space systems, and compatibility with various launch sites. A single concept and its subsystems were selected. Various alternatives for ISS mating; payload module and shroud design; solid rocket boosters; and guidance, navigation and control systems were examined and chosen. This design of the Peacekeeper SLV was verified probabilistically through a trajectory and orbit transfer analysis, as well as a trajectory optimization tool. Finally, the logistics and costs associated with the Peacekeeper SLV program were assessed.